JP2008095106A5 - - Google Patents
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- Publication number
- JP2008095106A5 JP2008095106A5 JP2007265189A JP2007265189A JP2008095106A5 JP 2008095106 A5 JP2008095106 A5 JP 2008095106A5 JP 2007265189 A JP2007265189 A JP 2007265189A JP 2007265189 A JP2007265189 A JP 2007265189A JP 2008095106 A5 JP2008095106 A5 JP 2008095106A5
- Authority
- JP
- Japan
- Prior art keywords
- high temperature
- temperature seal
- swelling
- short side
- matrix composite
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Claims (10)
内部領域(14)の被覆部の酸化スウェリングを実質的に防止する耐環境コーティング(22)
を備える高温シールであって、
耐環境コーティング(22)が内部領域(14)の外面に、1以上の突出部の遠位端が部分的に被覆されずに残り、残りの内部領域がコーティングで実質的に被覆されるように配置されている、高温シール。 Internal region comprising a least one projection that can be inserted into the ceramic matrix composite and a slot (32) in causing the swelling for oxidation is exposed to 500 ° C. greater than the high temperature environment (14), and inner region ( 14 ) Environmentally resistant coating ( 22 ) that substantially prevents oxidation swelling of the coating part
A high temperature seal comprising
The outer surface of the environmental barrier coating (22) is an internal region (14), remaining at the distal end of the at least one projection is not covered in part batchwise, so that the remaining interior region is substantially covered with a coating Located in the high temperature seal.
It occurs uncoated portion oxidation swelling of the projecting portion to be exposed to a high temperature environment of the window (52), having a predetermined size based on the swelling amount of the window (52) is desired protrusion claim 9, wherein High temperature seal.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/581,250 | 2006-10-16 | ||
US11/581,250 US7771159B2 (en) | 2006-10-16 | 2006-10-16 | High temperature seals and high temperature sealing systems |
Publications (3)
Publication Number | Publication Date |
---|---|
JP2008095106A JP2008095106A (en) | 2008-04-24 |
JP2008095106A5 true JP2008095106A5 (en) | 2012-10-18 |
JP5512076B2 JP5512076B2 (en) | 2014-06-04 |
Family
ID=38896150
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2007265189A Expired - Fee Related JP5512076B2 (en) | 2006-10-16 | 2007-10-11 | High temperature seal and high temperature seal system |
Country Status (4)
Country | Link |
---|---|
US (1) | US7771159B2 (en) |
EP (1) | EP1914454B1 (en) |
JP (1) | JP5512076B2 (en) |
CN (1) | CN101165374B (en) |
Families Citing this family (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20100061847A1 (en) * | 2008-09-09 | 2010-03-11 | General Electric Company | Steam turbine part including ceramic matrix composite (cmc) |
ES2718490T3 (en) * | 2010-07-26 | 2019-07-02 | Corts Eng Gmbh & Co Kg | Fluid Level Bearing Plate |
US8613451B2 (en) * | 2010-11-29 | 2013-12-24 | General Electric Company | Cloth seal for turbo-machinery |
FR2974401B1 (en) * | 2011-04-22 | 2013-06-14 | Commissariat Energie Atomique | METALLIC SEAL SEAL WITH CERAMIC WAVE |
US9534783B2 (en) * | 2011-07-21 | 2017-01-03 | United Technologies Corporation | Insert adjacent to a heat shield element for a gas turbine engine combustor |
US9353635B2 (en) | 2011-08-16 | 2016-05-31 | General Electric Company | Seal end attachment |
US9188228B2 (en) * | 2011-10-26 | 2015-11-17 | General Electric Company | Layered seal for turbomachinery |
US20130134678A1 (en) * | 2011-11-29 | 2013-05-30 | General Electric Company | Shim seal assemblies and assembly methods for stationary components of rotary machines |
US9587632B2 (en) | 2012-03-30 | 2017-03-07 | General Electric Company | Thermally-controlled component and thermal control process |
US9671030B2 (en) | 2012-03-30 | 2017-06-06 | General Electric Company | Metallic seal assembly, turbine component, and method of regulating airflow in turbo-machinery |
US9169567B2 (en) | 2012-03-30 | 2015-10-27 | General Electric Company | Components having tab members |
US9316109B2 (en) * | 2012-04-10 | 2016-04-19 | General Electric Company | Turbine shroud assembly and method of forming |
WO2014130147A1 (en) * | 2013-02-23 | 2014-08-28 | Jun Shi | Edge seal for gas turbine engine ceramic matrix composite component |
CA2900687C (en) * | 2013-03-05 | 2019-06-18 | Rolls-Royce Corporation | Structure and method for providing compliance and sealing between ceramic and metallic structures |
US9757920B2 (en) | 2013-03-15 | 2017-09-12 | Rolls-Royce Corporation | Flexible ceramic matrix composite seal |
US9719420B2 (en) * | 2014-06-02 | 2017-08-01 | General Electric Company | Gas turbine component and process for producing gas turbine component |
US9926790B2 (en) | 2014-07-21 | 2018-03-27 | Rolls-Royce Corporation | Composite turbine components adapted for use with strip seals |
US10281045B2 (en) | 2015-02-20 | 2019-05-07 | Rolls-Royce North American Technologies Inc. | Apparatus and methods for sealing components in gas turbine engines |
EP3088679A1 (en) | 2015-04-30 | 2016-11-02 | Rolls-Royce Corporation | Seal for a gas turbine engine assembly |
FR3036435B1 (en) | 2015-05-22 | 2020-01-24 | Safran Ceramics | TURBINE RING ASSEMBLY |
US9759079B2 (en) | 2015-05-28 | 2017-09-12 | Rolls-Royce Corporation | Split line flow path seals |
US20170030211A1 (en) * | 2015-07-28 | 2017-02-02 | General Electric Company | Seals with a conformable coating for turbomachinery |
US10458263B2 (en) | 2015-10-12 | 2019-10-29 | Rolls-Royce North American Technologies Inc. | Turbine shroud with sealing features |
US10301955B2 (en) | 2016-11-29 | 2019-05-28 | Rolls-Royce North American Technologies Inc. | Seal assembly for gas turbine engine components |
US10443420B2 (en) | 2017-01-11 | 2019-10-15 | Rolls-Royce North American Technologies Inc. | Seal assembly for gas turbine engine components |
US10577977B2 (en) | 2017-02-22 | 2020-03-03 | Rolls-Royce Corporation | Turbine shroud with biased retaining ring |
US10718226B2 (en) | 2017-11-21 | 2020-07-21 | Rolls-Royce Corporation | Ceramic matrix composite component assembly and seal |
FR3085708B1 (en) * | 2018-09-12 | 2020-11-27 | Safran Helicopter Engines | IMPROVED SEALING DEVICE FOR TURBOMACHINE ROTARY ASSEMBLY |
US20200095880A1 (en) * | 2018-09-24 | 2020-03-26 | United Technologies Corporation | Featherseal formed of cmc materials |
US11220924B2 (en) * | 2019-09-26 | 2022-01-11 | Raytheon Technologies Corporation | Double box composite seal assembly with insert for gas turbine engine |
US11519282B2 (en) | 2019-11-11 | 2022-12-06 | Raytheon Technologies Corporation | Ceramic matrix composite-based seal |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3322433A (en) * | 1964-03-10 | 1967-05-30 | Minnesota Rubber Co | Sealing ring and method of making same |
FR2724973B1 (en) * | 1982-12-31 | 1996-12-13 | Snecma | DEVICE FOR SEALING MOBILE BLADES OF A TURBOMACHINE WITH REAL-TIME ACTIVE GAME CONTROL AND METHOD FOR DETERMINING SAID DEVICE |
JPH053964Y2 (en) * | 1987-11-06 | 1993-01-29 | ||
JP2639674B2 (en) * | 1988-02-09 | 1997-08-13 | 三菱電線工業株式会社 | Gasket for engine exhaust system |
FR2635773B1 (en) * | 1988-08-31 | 1992-02-14 | Aerospatiale | COMPOSITE MATERIAL HAVING CARBON REINFORCING FIBERS AND MANUFACTURING METHOD THEREOF |
JP3303642B2 (en) * | 1995-03-30 | 2002-07-22 | 三菱自動車工業株式会社 | Heat storage type heat exchanger, heat-resistant sliding body used for the heat exchanger, etc. |
US6410148B1 (en) * | 1999-04-15 | 2002-06-25 | General Electric Co. | Silicon based substrate with environmental/ thermal barrier layer |
US6464456B2 (en) * | 2001-03-07 | 2002-10-15 | General Electric Company | Turbine vane assembly including a low ductility vane |
JP2003321277A (en) * | 2002-04-30 | 2003-11-11 | Ishikawajima Harima Heavy Ind Co Ltd | Ceramic-based composite material and method for producing the same |
US6893214B2 (en) | 2002-12-20 | 2005-05-17 | General Electric Company | Shroud segment and assembly with surface recessed seal bridging adjacent members |
US7004375B2 (en) * | 2003-05-23 | 2006-02-28 | National Starch And Chemical Investment Holding Corporation | Pre-applied fluxing underfill composition having pressure sensitive adhesive properties |
EP1484427A3 (en) * | 2003-06-06 | 2005-10-26 | General Electric Company | Top coating system for industrial turbine nozzle airfoils and other hot gas path components and related method |
US6942203B2 (en) * | 2003-11-04 | 2005-09-13 | General Electric Company | Spring mass damper system for turbine shrouds |
JP4470708B2 (en) * | 2004-11-22 | 2010-06-02 | 宇部興産株式会社 | Composite material and manufacturing method thereof |
US7238002B2 (en) * | 2005-11-03 | 2007-07-03 | General Electric Company | Damper seal system and method |
-
2006
- 2006-10-16 US US11/581,250 patent/US7771159B2/en not_active Expired - Fee Related
-
2007
- 2007-10-11 JP JP2007265189A patent/JP5512076B2/en not_active Expired - Fee Related
- 2007-10-12 EP EP07254046.1A patent/EP1914454B1/en not_active Not-in-force
- 2007-10-16 CN CN200710162674.1A patent/CN101165374B/en not_active Expired - Fee Related
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